What was found
CRACK ON SLAT PANEL NR 5 INNER SKIN BS XOS= 503 LT WING. DOUBLER WAS FABRICATED, TREATED AND PAINTED , INSTALLED IAW SRM 57-01, FIG 3, 51-10-3, 51-30-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SLAT PANEL NR 5 INNER SKIN BS XOS= 503 LT WING. DOUBLER WAS FABRICATED, TREATED AND PAINTED , INSTALLED IAW SRM 57-01, FIG 3, 51-10-3, 51-30-8.